Skip to content

Home/Archive/NASA NTRS

NASA NTRS · 19630026593

THEORETICAL AND EXPERIMENTAL MODELS FOR UNSTABLE ROCKET COMBUSTOR

View original source ↗Export metadata ↓

Abstract

Theoretical and experimental models of the study of combustion instability in rocket combustors

Explore related subjects

ROCKET COMBUSTOR COMBUSTION INSTABILITY

Keep this discovery

Explore connections, maps & timelines

Priem, R. J.. 1963-01-01. THEORETICAL AND EXPERIMENTAL MODELS FOR UNSTABLE ROCKET COMBUSTOR. https://ntrs.nasa.gov/citations/19630026593

Cite the original work for its findings. Save a collection to share your selection of sources.

KEEP EXPLORING

Related reports

NASA NTRS1967

Chamber shape effects on combustion instability

Rocket combustor shape effects on combustion instability

ROCKET COMBUSTOR↗

NASA NTRS1966

Analysis of n-heptane vaporization in unstable combustor with traveling transverse oscillations

Vaporization analysis of n-heptane in unstable combustor with traveling transverse oscillations using drop-evaporation theory

ROCKET COMBUSTOR↗

NASA NTRS1965

Evaluation of absorption liners for suppression of combustion instability in rocket engines.

Acoustic absorption liners for suppressing HF COMBUSTION instability in rocket engine combustion chambers

ROCKET COMBUSTOR↗